DRAINING BRAKE SYSTEM.
To drain the brake system, connect a hose to the bleeder fitting on the bottom of the cylinder and place the
other end of the line in a suitable container. Open the bleeder and slowly pump the hand brake lever and the
desired brake pedal until fluid ceases to flow. To drain the wheel brake unit, disconnect the line at the bottom of
the unit and allow fluid to flow into a suitable container. To clean the brake system, flush with denatured alcohol.
TIRES.
pressure examine the tires for wear, cuts, bruises and slippage. The tire, tube, and wheel should be balanced
when installed. Align the index mark on the tire with the index mark on the tube.
TIRE BALANCE.
Proper balancing is critical for the life of aircraft tires. If a new tire is balanced upon installation it will usually
remain balanced for the life of the tire without having any shimmy or flat spots. and an inexpensive balancer can
be made that will balance almost any tire for light aircraft. Refer to Chapter 91 for balancer details. Balance the
tire as follows:
1. Mount the tire and tube (if one is used) on the wheel, but do not install the securing bolts. Install the
wheel bearings in the wheel; then, using the -7 bushings, -6 spacers, and -5 nuts, install the wheel-tire
assembly on the -8 pipe. Secure the -5 nuts finger-tight so that the wheel halves touch each other. Be
sure the bolt holes are aligned. Insert the -4 axle through the -8 pipe and place the wheel in the center of
the balancer. Make sure the axle is only on the chamfered edges of the balancer and that it is at 90° to the
sides of the balancer.
2. Release the tire. If it is out of balance it will rotate, coming to rest with the heaviest point on the bottom.
Tape a 1/2 ounce patch across top center of the tire. Rotate the tire 45° and release it again. If the tire
returns to the same position, add a 1 ounce patch and again rotate the tire and release it. Continue this
procedure until the tire is balanced.
3. When balance is attained, put a chalk mark on the sidewall directly below the patch. Use one mark for
each half ounce of weight needed. Mark the valve stem location on the tire and the opposite wheel half
to assure reassembly in the same position. Remove the wheel from the balance stand, break it down and
clean the inside of the tire with toluol. Apply a coat of patch cement to both the patch and the inside
center of the tire in line with the chalk marks. When the cement has dried, install the patches making
certain they are on the center line of the tire and aligned with the chalk marks on the sidewall. Burnish
the patches to remove trapped air, etc.
4. When reassembling the wheel, powder the inside of the tire. Mount the tire on the valve side of the
wheel in the same position it was in when it was balanced. Install the other wheel half, aligning the chalk
marks. Install the bolts and tighten to required torque, then air the tire and recheck the balance. The
wheel should not be more than 1/ 2 ounce out of balance.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
1 2 - 2 3 - 0 1
Page 12-08
Revised: May 15, 1989
1D8
PIPER AIRCRAFT
Содержание SEMINOLE PA-44-180
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Страница 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
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Страница 49: ...CHAPTER LIFTING AND SHORING 1C1...
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Страница 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
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Страница 58: ...CHAPTER TOWING AND TAXIING 1C10...
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Страница 62: ...CHAPTER PARKING AND MOORING 1C14...
Страница 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Страница 70: ...CHAPTER SERVICING 1C22...
Страница 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Страница 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Страница 189: ...CHAPTER AUTOFLIGHT 1H21...
Страница 192: ...CHAPTER COMMUNICATIONS 1H24...
Страница 202: ...CHAPTER ELECTRICAL POWER 1I10...
Страница 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Страница 233: ...CHAPTER FIRE PROTECTION 1J17...
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Страница 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Страница 304: ...2A18 CHAPTER FUEL...
Страница 325: ...2B17 CHAPTER HYDRAULIC POWER...
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Страница 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
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Страница 414: ...CHAPTER LANDING GEAR 2F13...
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Страница 479: ...2I6 CHAPTER LIGHTS...
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Страница 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Страница 503: ...2J7 CHAPTER OXYGEN...
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Страница 524: ...2K6 CHAPTER VACUUM...
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Страница 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
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Страница 547: ...2L7 CHAPTER STRUCTURES...
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Страница 582: ...CHAPTER DOORS 3A18...
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Страница 593: ...CHAPTER STABILIZERS 3B8...
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Страница 604: ...CHAPTER WINDOWS 3B22...
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Страница 611: ...CHAPTER WINGS 3C10...
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Страница 624: ...CHAPTER PROPELLER 3D1...
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Страница 643: ...CHAPTER POWER PLANT 3D21...
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Страница 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
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Страница 681: ...CHAPTER IGNITION 3F16...
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Страница 712: ...CHAPTER ENGINE INDICATING 3H1...
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Страница 730: ...CHAPTER EXHAUST 3H19...
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Страница 734: ...CHAPTER OIL 3I1...
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Страница 743: ...CHAPTER STARTING 3I11...
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Страница 755: ...CHAPTER TURBINES 3J1...
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Страница 787: ...CHAPTER CHARTS AND WIRING DIAGRAMS 4A18...
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